Thank you for taking an interest in our selection of 5365-01-543-1422 parts here on Boost AOG. You are currently on the RFQ form for part number 54542, a Eaton Corporation product listed with the Bushing Machine Thread If part number 54542 catches your eye, be sure to use our online RFQ service to request quotes, with customized responses provided within 15 minutes of us receiving and reviewing a completed submission.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5365-01-543-1422 Item PartTypeName: BUSHING,MACHINE THREAD | 5365 | 015431422 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 54542 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAJF | THREAD DIRECTION | RIGHT-HAND |
| AATA | COUNTERSINK ANGLE IN DEG | 45.0 |
| ABHP | OVERALL LENGTH | 0.640 INCHES MINIMUM AND 0.660 INCHES MAXIMUM |
| ABNM | THICKNESS | 0.120 INCHES MINIMUM AND 0.140 INCHES MAXIMUM |
| ADBD | COUNTERSINK DEPTH | 0.025 INCHES MINIMUM AND 0.040 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| AJYR | SCREW THREAD LENGTH | 0.370 INCHES NOMINAL |
| ASDB | WIDTH ACROSS FLATS | 0.970 INCHES MINIMUM AND 1.030 INCHES MAXIMUM |
| BQDD | COUNTERSINK LOCATION | THREADED END AND WRENCHING END |
| BXBR | HOLE INSIDE DIAMETER | 0.765 INCHES MINIMUM AND 0.785 INCHES MAXIMUM |
| CMLP | THREAD QUANTITY PER INCH | 18 |
| CQJX | NOMINAL THREAD SIZE | 1.063 INCHES |
| CTTC | THREAD TOLERANCE CLASS | 3A EXTERNAL |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | RETAINER NUT |
| FEAT | SPECIAL FEATURES | THREADS ARE UNJEF SERIES; HAS A 0.150 WIDE GROVE LOCATED ABOVE THE THREADS, DIA OF GROVE AREA 0.971 TO 0.981; CONTAINS 2 LOCKWIRE HOLES 0.046 DIA LOCATED 180 DEG APART IN THE WRENCHING FACLITY END, 0.065 FROM THE TOP EDGE AND 0.078 FROM THE |
| MATT | MATERIAL | ALUMINUM ALLOY 6061 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | SAE-AMS-QQ-A-225/8 FED SPEC SINGLE MATERIAL RESPONSE |
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